Spitzer's Spacecraft Bus
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Final Installation of the Spacecraft Harness Lockheed Martin |
Spitzer's Spacecraft Bus is an octagonal structure in which the avionics and
the science instrument warm electronics are housed. The Spacecraft Bus
provides electrical power to the science instruments, orients and stabilizes
the boresight of the telescope, collects and compresses data from the
science instruments for later transmission to the ground, executes stored
commands to direct science instrument activities, and communicates with
the ground system.
The bus structure makes up the nine bays within which the bus equipment is
housed. Four side modules, four corner modules, two heatpipe equipment
panels, and six equipment panels make up the nine bays. The equipment
panels are sandwiched between the modules and are bolted and bonded
together for maximum stiffness and structural integrity. On the outside of the
bays, panels are bolted to the modules. These panels are removable and
provide access to the outer bays during integration and test. The center bay
is accessible from the top.
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| Spacecraft Bus Structure |
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| Interior of the Spacecraft Bus |
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